A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. It consists of disks, blades, hubs, and the like. It is the moving part of a turbine assembly, aircraft gas turbine engine. It has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 6130-01-316-6457
NSN 5925-01-020-7706
NSN 5905-01-266-0856
NSN 2925-00-091-6745
NSN 5925-01-452-7070
NSN 5985-00-419-8705
NSN 5999-00-782-5323
NSN 6685-01-226-8645
NSN 6685-00-008-0660
NSN 5975-01-413-7840
NSN 5925-00-140-0009
NSN 5945-01-126-4998